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Inventor profile of:

Robert E. Malecki

City:

Storrs, Connecticut

Country:

United States

Published Applications:

Last publication date:

2022-05-05

Top Assignees for applications by Robert E. Malecki

The entities that hold a legal rights for patent applications filed by inventor Malecki Robert E.:

UNITED TECHNOLOGIES CORPORATION 16 Farmington, CT United States
UNITED TECHNOLOGIES CORPORATION 8 Hartford, CT United States
Raytheon Technologies Corporation 4 Farmington, CT United States
RTX Corporation 4 Farmington, CT United States
United Technologies Corporation 1 Framington, CT United States

Recent patent applications by Malecki Robert E.

Robert E. Malecki from Storrs, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2022-05-05

US20220136441A1

Mechanical engineering

Gas turbine engine mounted above wing and with camber

#2 | 2022-05-05

US20220136440A1

Mechanical engineering

GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

#3 | 2022-01-13

US20220010689A1

Mechanical engineering

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#4 | 2021-09-16

US20210285403A1

Mechanical engineering

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#5 | 2020-02-27

US20200063603A1

Mechanical engineering

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE

#6 | 2020-01-23

US20200025036A1

Mechanical engineering

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#7 | 2019-09-05

US20190271269A1

Mechanical engineering

Elongated geared turbofan with high bypass ratio

#8 | 2019-01-17

US20190017470A1

Mechanical engineering

Convergent divergent exit nozzle for a gas turbine engine

#9 | 2018-07-26

US20180209379A1

Mechanical engineering

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#10 | 2018-06-14

US20180163568A1

Mechanical engineering

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#11 | 2017-10-19

US20170298954A1

Mechanical engineering

Nacelle short inlet

#12 | 2017-10-12

US20170292882A1

Physics

Nacelle deflection measurement assembly

#13 | 2017-07-06

US20170190438A1

Performing operations; transporting

Nacelle short inlet for fan blade removal

#14 | 2016-08-18

US20160237856A1

Mechanical engineering

Track fairing assembly for a turbine engine nacelle

#15 | 2016-07-28

US20160215732A1

Mechanical engineering

BYPASS DUCT HEAT EXCHANGER PLACEMENT

#16 | 2016-07-14

US20160201570A1

Mechanical engineering

Exhaust nozzle arrangement for geared turbofan

#17 | 2016-07-14

US20160201569A1

Mechanical engineering

Exhaust nozzle arrangement for geared turbofan

#18 | 2016-07-07

US20160195038A1

Mechanical engineering

Convergent divergent exit nozzle for a gas turbine engine

#19 | 2016-04-21

US20160108854A1

Mechanical engineering

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE

#20 | 2016-03-17

US20160076460A1

Mechanical engineering

Nacelle and compressor inlet arrangements

#21 | 2016-03-03

US20160061057A1

Mechanical engineering

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#22 | 2016-01-07

US20160003194A1

Mechanical engineering

Asymmetric fan nozzle in high-BPR separate-flow nacelle

#23 | 2016-01-07

US20160003091A1

Mechanical engineering

NACELLE INTERNAL AND EXTERNAL FLOW CONTROL

#24 | 2015-09-03

US20150247425A1

Mechanical engineering

Non-circular aft nacelle cowling geometry

#25 | 2015-02-12

US20150044028A1

Mechanical engineering

Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

#26 | 2014-09-25

US20140286754A1

Mechanical engineering

Exhaust nozzle for an elongated gear turbofan with high bypass ratio

#27 | 2014-09-25

US20140283501A1

Mechanical engineering

Elongated geared turbofan with high bypass ratio

#28 | 2014-09-04

US20140246514A1

Mechanical engineering

Turbomachine thrust reverser

#29 | 2014-08-07

US20140216005A1

Mechanical engineering

Gas Turbine Engine Assembly Including A Thrust Reverser

#30 | 2013-12-05

US20130319002A1

Mechanical engineering

Nacelle bifurcation for gas turbine engine

#31 | 2013-08-29

US20130221124A1

Mechanical engineering

Gas turbine engine thrust reverser system

#32 | 2011-10-06

US20110243719A1

Mechanical engineering

Non-circular aft nacelle cowling geometry

InventorID:

409285 ⎘